Stainless Steel 347H – DatasheetStainless Steel 347H – DatasheetStainless Steel 347H – DatasheetStainless Steel 347H – Datasheet

STAINLESS STEEL GRADE 347H (UNS S34709) — COMPREHENSIVE TECHNICAL DATASHEET

Stainless Steel Grade 347H (UNS S34709) is a high-carbon, niobium-stabilized austenitic stainless steel optimized for service environments characterized by elevated thermal exposure and highly corrosive process streams. As the high-carbon variant of the standard Grade 347 alloy, Grade 347H is specifically engineered to maintain long-term structural stability, enhanced creep resistance, and exceptional high-temperature tensile durability.

The primary metallurgical advantage of Grade 347H is its resistance to sensitization—the precipitation of chromium carbides ($Cr_{23}C_{6}$) at grain boundaries inside the critical thermal window of 427°C to 816°C (800°F to 1500°F). The stoichiometric addition of niobium preferentially forms fine, dispersed niobium carbides ($NbC$) within the grains, actively trapping carbon atoms and preserving chromium solid-solution levels to ensure continuous passivity along the grain boundaries.

■ International Standards & Cross-Referencing

The carbon limits of Grade 347H are strictly controlled between 0.04% and 0.10%. Dual certification with standard Grade 347 is achieved when the carbon content falls precisely between 0.04% and 0.08%, allowing elements to meet both low-temperature corrosion boundaries and premium high-temperature creep thresholds.

Standard Body Designation Code Equivalent Grade / Specification
UNS (USA)S34709Grade 347H
EN (European Union)1.4961X6CrNiNb18-12
DIN (Germany)1.4961X8CrNiNb16-13
AFNOR (France)—Z6CNNb18-10
JIS (Japan)SUS 347H—
GOST (Russia)—08KH18N12B
GB (China)—1Cr18Ni11Nb

■ Chemical Composition Limits (Weight %)

Element Grade 347H (UNS S34709) Standard 347 (UNS S34700) Primary Metallurgical Significance
Carbon (C)0.040 – 0.1000.080 maxElevated content ensures intra-granular carbide precipitation for dislocation pinning.
Chromium (Cr)17.00 – 19.0017.00 – 19.00Establishes the passive chromia ($Cr_2O_3$) film for scaling protection.
Nickel (Ni)9.00 – 13.009.00 – 13.00Stabilizes the FCC matrix; increases toughness and thermal shock resistance.
Niobium (Nb)$8 \times \text{C}$ min – 1.00 max$10 \times \text{C}$ min – 1.00 maxActs as a powerful stabilizing agent, preventing intergranular decay.
Manganese (Mn) max2.0002.000Deoxidizer; enhances nitrogen solubility and preventive matrix consolidation.
Silicon (Si) max0.750*0.750Capped to reduce the rate of brittle intermetallic phase formation at intermediate heat.
Phosphorus (P) max0.0450.045Restricted impurity to control hot cracking tendencies during welding.
Sulfur (S) max0.0300.030Restricted to avoid low-melting-point boundary segregations.
Iron (Fe)BalanceBalanceBase substrate metal matrix.

* Note: Silicon limit is relaxed to 1.00% maximum for structural tubing and forged configurations under ASTM A182.

■ Proprietary Datasheet Download

For principal piping designers, boiler specialists, and procurement officials requiring comprehensive engineering metrics, finite element strain logs, and code-compliance certifications, the unified datasheet must be accessed.

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Alloy 347H — Complete Technical Yield, Creep & Manufacturing Datasheet

Contains empirical material matrices, long-term activation logs, and complete stress relaxation cracking prevention parameters. Corporate credentials required.

⬇ DOWNLOAD DATASHEET

■ Physical Constants and Thermophysical Values

Due to its highly alloyed FCC matrix, Grade 347H exhibits low thermal conductivity (roughly 30% that of mild structural carbon steel) paired with elevated coefficients of thermal expansion. These parameters dictate transient thermal stresses.

Physical Property Value in Metric / SI Units Value in Imperial / US Units
Density (Ambient Base)7.96 g/cm³0.288 lb/in³
Melting Range Limits1398°C – 1446°C2550°F – 2635°F
Modulus of Elasticity (20°C)193 GPa28.0 × 10⁶ psi
Poisson's Ratio0.27 – 0.300.27 – 0.30
Specific Heat Capacity (0-100°C)500 J/kg·K0.120 BTU/lb·°F
Shear Modulus77 GPa11.2 × 10⁶ psi
Electrical Resistivity (20°C)72 μΩ·cm2.83 × 10⁻⁵ Ω·inch
Relative Magnetic Permeability1.008 (Annealed)1.008 (Annealed)

The non-linear tracking of thermophysical properties across an escalating thermal service range is summarized below:

Service Temperature (°C / °F) Linear Coefficient of Thermal Expansion (μm/m·°C) Thermal Conductivity (W/m·K) Electrical Resistivity (μΩ·cm) Modulus of Elasticity (GPa / Mpsi)
20°C / 68°F—14.272193 / 28.0
100°C / 212°F16.0 (20-100°C range)16.378188 / 27.2
400°C / 752°F17.8 (20-260°C range)19.5100165 / 23.9
500°C / 932°F18.4 (20-540°C range)21.4106158 / 22.9
600°C / 1112°F18.9 (20-600°C range)22.8112150 / 21.7
1000°C / 1832°F20.5 (20-1000°C range)——120 / 17.4 (Est.)

■ Room-Temperature Mechanical Property Requirements

At ambient limits, the solution-treated matrix balances robust yield performance with excellent cold-deforming reserves and fracture resilience.

Product Standard / Form Yield Strength Rp0.2 Tensile Strength Rm Min. Elongation (in 50 mm) Hardness Boundaries (max)
ASTM A240 Plate (UNS S34709)≥ 205 MPa (30 ksi)≥ 515 MPa (75 ksi)35% – 40%201 HBW / 95 HRB
ASTM A182 Forgings (UNS S34709)≥ 205 MPa (30 ksi)≥ 515 MPa (75 ksi)30%187 HBW (RA ≥ 50%)
EN 1.4961 Bars / Shapes≥ 200 MPa510 – 750 MPa35% (Axial)192 HBW

■ Short-Term Elevated Temperature Tensile Limits

These values guide stress equations during transient, non-equilibrium pressure excursions across processing plants before creep runtime limits take over.

Operating Temperature 0.2% Yield Strength (MPa / ksi) 1.0% Yield Strength (MPa / ksi) Ultimate Tensile Strength (MPa / ksi)
100°C / 212°F175 / 25.4210 / 30.5450 / 65.3
300°C / 572°F139 / 20.2167 / 24.2415 / 60.2
500°C / 932°F124 / 18.0155 / 22.5385 / 55.8
600°C / 1112°F112 / 16.2148 / 21.5345 / 50.0
700°C / 1292°F98 / 14.2132 / 19.1240 / 34.8

■ Long-Term Creep Rupture Strength (Solution-Annealed)

At continuous structural exposure above 600°C, vacancy diffusion paths dominate. Fine, coherent intra-granular niobium carbonitride ($Nb(C,N)$) precipitates act as pinning centers that lock dislocation glide, significantly lowering the secondary minimum creep rate.

Temperature Stress for Rupture at 10,000 Hours Stress for Rupture at 100,000 Hours
540°C / 1004°F253 MPa (36.7 ksi)186 MPa (27.0 ksi)
580°C / 1076°F192 MPa (27.8 ksi)135 MPa (19.6 ksi)
600°C / 1112°F166 MPa (24.1 ksi)115 MPa (16.7 ksi)
650°C / 1202°F112 MPa (16.2 ksi)74 MPa (10.7 ksi)
700°C / 1292°F74 MPa (10.7 ksi)48 MPa (7.0 ksi)
800°C / 1472°F28 MPa (4.1 ksi)16 MPa (2.3 ksi)

■ ASME Section II Part D Maximum Allowable Stress Comparison

The performance gap in allowable working stress illustrates the higher temperature capacity achieved by the niobium stabilization chemistry of Grade 347H over titanium-stabilized alternatives in the creep-governed design regime.

Operating Temperature SA182 F347H Allowable Stress (MPa / ksi) SA182 F321H Allowable Stress (MPa / ksi) High-Temperature Strength Performance Gap
100°C / 212°F160 / 23.2150 / 21.8Short-term yield limits rule both lines.
500°C / 932°F125 / 18.1110 / 16.0Grade 347H exhibits an ≈ 13.6% strength premium.
600°C / 1112°F115 / 16.7100 / 14.5Grade 347H exhibits an ≈ 15.1% strength premium.

■ Environmental Compatibility & Aqueous Limits

  • Polythionic Acid Stress Corrosion Cracking (PTA-SCC): Outstanding resistance in sulfur-bearing refinery streams. Niobium binding prevents intergranular carbide precipitation during continuous processing, eliminating localized chromium-depleted zones. This allows 347H to completely resist PTA-SCC during moist downtime blocks without mandatory post-weld chemical stabilization.
  • Isothermal vs. Cyclic Gas Oxidation: Safe up to 850°C (1562°F) in continuous dry air, and up to 750°C (1382°F) in continuous steam runs. Thermal cycling induces interfacial shear stresses due to the high expansion mismatch ($\alpha \approx 20.5 \times 10^{-6}/\text{K}$ at 1000°C), which can fracture the protective chromia film.
  • Halide/Chloride Pitting Restrictions: Lacking molybdenum additions, the alloy's pitting resistance equivalent number is limited ($\text{PREN} \approx 18$). Prone to localized crevice activation and stress corrosion cracking in chloride-bearing fluids at service environments exceeding 60°C (140°F). Avoid reducing mineral acids like active sulfuric lines.

■ Welding Metallurgy and Stress Relaxation Cracking (SRC)

Grade 347H exhibits excellent fusion weldability, but fully austenitic weld zones are highly susceptible to hot cracking (micro-fissuring) due to low impurity solubility along liquid boundaries. Heat inputs must be kept low, and interpass temperatures must remain below 150°C (302°F) to ensure the weld metal solidifies with a protective delta-ferrite content within a 5 to 13 FN (Ferrite Number) range.

The Mechanics of SRC (Reheat Cracking): Highly constrained, thick-walled weld joints ($\ge 25.4 \text{ mm}$ / 1.0 inch thickness) are highly vulnerable to delayed intergranular cracking when placed into thermal service above 540°C. In the high-heat HAZ adjacent to the fusion boundary, pre-existing niobium carbides dissolve completely. Upon reheating, they re-precipitate as extremely fine, coherent intra-granular $Nb(C,N)$ particles, strengthening the grain interiors. Consequently, residual welding stresses concentrate entirely along the weaker grain boundaries, leading to rapid creep cavitation and sudden brittle fracture.

■ Structural Design & Procurement Recommendations

  • Grain Size Enforcement Boundary: When requesting material for creep-critical application lines, purchase specs must mandate an actual carbon content of 0.04% to 0.10% and require a certified ASTM E112 grain size of No. 7 or coarser. Dual-certified 347/347S items must be audited to verify they meet these criteria; otherwise, grain boundary vacancy sliding will cause premature creep collapse.
  • Mitigating SRC via PWHT: For thick, highly constrained joints, mitigate stress relaxation cracking by enforcing a rapid post-weld heat treatment. Weldments must be heated quickly through the critical precipitation window ($500^\circ\text{C} - 800^\circ\text{C}$) to a peak stress-relief range of 900°C to 950°C, allowing bulk residual stress relaxation to occur before coherent intra-granular strain aging locks the matrix. Alternatively, specify ductile AWS E16.8.2 weld consumables to absorb shrinkage strain safely.
  • Processing Safety Limits: The work-hardening rate is high ($\approx 14 \text{ MPa per } 1\%$ reduction of area). Severe cold bending must be completed in stages with intermediate annealing steps. Machining parameters must employ continuous positive feeds; tool riding or dwell will cause rapid surface glazing, resulting in premature tool failure.
  • Smelting Optimization: For high-pressure utility boiler loops or aerospace exhaust manifolds exposed to extreme pressure and corrosive salts, specify secondary Electro Slag Remelting (ESR) or Protective Atmosphere Electro Slag Remelting (PESR) processing to minimize inclusion density and ensure elemental homogeneity.

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